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Aug 14, 2020 at 15:28 vote accept StarshipGood
Jun 20, 2020 at 9:00 history tweeted twitter.com/StackSpaceExp/status/1274265790758477830
Jun 9, 2020 at 21:06 answer added A McKelvy timeline score: 6
Jun 8, 2020 at 16:25 comment added Anton Hengst @CarlWitthoft How were those optimum thrust/weight ratios determined in the first place?
Jun 8, 2020 at 16:23 comment added Anton Hengst This is a valid problem even if poorly written. "How to model a liquid combustion engine" is a very big question, but it can be answered. Ponomarenko (2009) provides a very broad overview, including much more of the non-combustion considerations that I do not cover in my answer. 87.106.90.141/downloads/1.0/docs/…
Jun 8, 2020 at 16:18 answer added Anton Hengst timeline score: 3
Jun 8, 2020 at 15:29 comment added Carl Witthoft Why would you change a mixture ratio away from optimum thrust: weight ratio?
Jun 8, 2020 at 12:43 review Close votes
Jun 8, 2020 at 18:14
Jun 8, 2020 at 12:41 history edited Organic Marble
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Jun 8, 2020 at 12:27 comment added Organic Marble You will need to be more specific. Right now this says 'teach me to compute every kind of engine parameter'. for example, pick one parameter and say what you want to vary to see the effect.
Jun 8, 2020 at 8:04 review First posts
Jun 8, 2020 at 8:34
Jun 8, 2020 at 7:58 history asked StarshipGood CC BY-SA 4.0